making consistent with the website

Author: planes

Solar_UAV_Optimization/Missions.py

@@ -57,7 +57,7 @@ def mission(analyses,vehicle):
     # segment attributes     
     segment.state.numerics.number_control_points = 50
     segment.dynamic_pressure = 115.0 * Units.pascals
-    segment.start_time       = time.strptime("Tue, Jun 21  11:00:00  2017", "%a, %b %d %H:%M:%S %Y",)
+    segment.start_time       = time.strptime("Tue, Jun 21  11:00:00  2020", "%a, %b %d %H:%M:%S %Y",)
     segment.altitude         = 1000.0 * Units.feet
     segment.distance         = 1000.0 * Units.km
     segment.charge_ratio     = 1.0

tut_mission_B737.py

@@ -582,7 +582,7 @@ def configs_setup(vehicle):
     config.tag = 'cutback'
     config.wings['main_wing'].control_surfaces.flap.deflection = 20. * Units.deg
     config.wings['main_wing'].control_surfaces.slat.deflection = 20. * Units.deg
-    config.max_lift_coefficient_factor    = 1. #0.95
+    config.max_lift_coefficient_factor    = 1.
 
     configs.append(config)    
 
@@ -595,7 +595,7 @@ def configs_setup(vehicle):
 
     config.wings['main_wing'].control_surfaces.flap.deflection = 30. * Units.deg
     config.wings['main_wing'].control_surfaces.slat.deflection = 25. * Units.deg  
-    config.max_lift_coefficient_factor    = 1. #0.95
+    config.max_lift_coefficient_factor    = 1. 
 
     configs.append(config)
 
@@ -608,7 +608,7 @@ def configs_setup(vehicle):
 
     config.wings['main_wing'].control_surfaces.flap.deflection = 20. * Units.deg
     config.wings['main_wing'].control_surfaces.slat.deflection = 20. * Units.deg
-    config.max_lift_coefficient_factor    = 1. #0.95
+    config.max_lift_coefficient_factor    = 1. 
 
     configs.append(config)
 

tut_solar_uav.py

@@ -412,7 +412,7 @@ def mission_setup(analyses,vehicle):
 
     # segment attributes     
     segment.state.numerics.number_control_points = 64
-    segment.start_time     = time.strptime("Tue, Jun 21 11:30:00  2017", "%a, %b %d %H:%M:%S %Y",)
+    segment.start_time     = time.strptime("Tue, Jun 21 11:30:00  2020", "%a, %b %d %H:%M:%S %Y",)
     segment.altitude       = 15.0  * Units.km 
     segment.mach           = 0.12
     segment.distance       = 3050.0 * Units.km